Flight Dynamics Modeling and Simulation of a Damaged Transport Aircraft
Flight Dynamics Modeling and Simulation of a Damaged Transport Aircraft
- Neue Suche nach: G. H. Shah
- Neue Suche nach: M. A. Hill
- Neue Suche nach: G. H. Shah
- Neue Suche nach: M. A. Hill
A study was undertaken at NASA Langley Research Center to establish, demonstrate, and apply methodology for modeling and implementing the aerodynamic effects of MANPADS damage to a transport aircraft into real-time flight simulation, and to demonstrate a preliminary capability of using such a simulation to conduct an assessment of aircraft survivability. Key findings from this study include: superpositioning of incremental aerodynamic characteristics to the baseline simulation aerodynamic model proved to be a simple and effective way of modeling damage effects; the primary effect of wing damage rolling moment asymmetry may limit minimum airspeed for adequate controllability, but this can be mitigated by the use of sideslip; combined effects of aerodynamics, control degradation, and thrust loss can result in significantly degraded controllability for a safe landing; and high landing speeds may be required to maintain adequate control if large excursions from the nominal approach path are allowed, but high-gain pilot control during landing can mitigate this risk.
Dokumentinformationen
Flight Dynamics Modeling and Simulation of a Damaged Transport Aircraft
2012
12 pages
Report
Keine Angabe
Englisch
Aircraft , Test Facilities & Equipment , Damage , Flight simulation , Transport aircraft , Real time operation , Portable equipment , Air defense , Wind tunnel tests , Wings , Dynamic characteristics , Aircraft models , Rolling moments , Damping tests , Controllability , Landing speed , Sideslip , Airspeed
Ähnliche Titel
Flight Dynamics Modeling and Simulation of a Damaged Transport Aircraft
| British Library Conference Proceedings | 2012
Flight Dynamics and Hybrid Adaptive Control of Damaged Aircraft
| Online Contents | 2008
ERRATUM - Flight Dynamics and Hybrid Adaptive Control of Damaged Aircraft
| Online Contents | 2008